@inproceedings{oai:jaxa.repo.nii.ac.jp:00038250,
 author = {高橋, 政浩 and 冨田, 健夫 and 坂本, 博 and 田村, 洋 and 渡辺, 泰秀 and 坪井, 正徳 and Takahashi, Masahiro and Tomita, Takeo and Sakamoto, Hiroshi and Tamura, Hiroshi and Watanabe, Yasuhide and Tsuboi, Masanori},
 book = {航空宇宙技術研究所特別資料: 航空宇宙数値シミュレーション技術シンポジウム2002論文集, Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2002},
 month = {Mar},
 note = {Axisymmetric computation was applied to the transient flow in a sub-scaled LE-7A nozzle with three different configurations of a joint section between its upper nozzle and nozzle extension sections, such as a backward facing step for film-cooling, to investigate the influences of the flow disturbances produced by such nozzle surface shapes on the transient flow characteristics and to examine the possible cause of side-loads observed in the experiments. Rapid movement of the separation point occurred when it passed through the joint section. One of reasons for the occurrence of a highly asymmetrical flow causing large side-load is considered to be that the location of the separation point becomes very sensitive to the flow condition when the separation point passes through the joint section., 資料番号: AA0045948029, レポート番号: NAL SP-57},
 pages = {160--165},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {ロケットエンジンノズル形状と横力の発生について},
 volume = {57},
 year = {2003}
}